Analyses incorporating the gravitational effects of Earth to calculate optimal impulses for deflecting Earth-crossing asteroids are presented. The patched conic method is used to formulate the constrained optimization problem. Geocentric constraints are mapped to heliocentric variables by the use of the impact parameter. The result is a unified nonlinear programming problem in the sense that no distinctions are made for short or long warning times. Numerical solutions indicate that the ΔV requirements are considerably more than those or the previously published two-body analysis that excluded third-body effects. Generally speaking, the increments in the minimum ΔV due to the gravitational effects of the Earth are large (by as much as 60%) for near-Earth asteroids, and the errors diminish for orbits with large eccentricities (e > 0.7). Some interesting results for short warning times are also discussed.
|Number of pages||6|
|Journal||Journal of Spacecraft and Rockets|
|Publication status||Published - 2001 Sept|
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science